Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Nándor Terkovics"'
Publikováno v:
Terkovics, N, Neild, S A, Lowenberg, M, Szalai, R & Krauskopf, B 2016, ' Substructurability : The effect of interface location on a real-time dynamic substructuring test ', Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, vol. 472, no. 2192, 20160433 . https://doi.org/10.1098/rspa.2016.0433
Proceedings. Mathematical, Physical, and Engineering Sciences / The Royal Society
Proceedings. Mathematical, Physical, and Engineering Sciences / The Royal Society
A full-scale experimental test for large and complex structures is not always achievable. This can be due to many reasons, the most prominent one being the size limitations of the test. Real-time dynamic substructuring is a hybrid testing method wher
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1b256635b05f66f4d9cfc944b49326c0
https://research-information.bris.ac.uk/ws/files/83659437/20160433.full.pdf
https://research-information.bris.ac.uk/ws/files/83659437/20160433.full.pdf
Publikováno v:
Terkovics, N, Neild, S A, Lowenberg, M H & Krauskopf, B 2014, ' Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System ', Journal of Aircraft, vol. 51, no. 1, pp. 259-272 . https://doi.org/10.2514/1.C032324
Terkovics, N, Neild, S A, Lowenberg, M H & Krauskopf, B 2014, ' Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System ' AIAA Journal, vol 51, no. 1, pp. 259-272 ., 10.2514/1.C032324
Terkovics, N, Neild, S A, Lowenberg, M H & Krauskopf, B 2014, ' Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System ' AIAA Journal, vol 51, no. 1, pp. 259-272 ., 10.2514/1.C032324
Under certain conditions during takeoff and landing, pilots may sometimes experience vibrations in the cockpit. Because the cockpit is located right above the nose landing gear, which is known to potentially be prone to self-excited vibrations at cer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b0b22b164a2e91bf7012dc0c3efea23c
https://research-information.bris.ac.uk/en/publications/0eb769f0-e1c0-4236-bee6-1a0779f2eea9
https://research-information.bris.ac.uk/en/publications/0eb769f0-e1c0-4236-bee6-1a0779f2eea9
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
Under certain conditions during takeoff and landing, pilots may sometimes experience vibrations in the cockpit. Because the cockpit is located right above the nose landing gear, which is known to potentially be prone to self-excited vibrations at cer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::55fe52d005a8ef1698f802a0fdd005d4
https://doi.org/10.2514/6.2012-4731
https://doi.org/10.2514/6.2012-4731
